GB289427A - Improvements in radial gas- or steam turbines - Google Patents
Improvements in radial gas- or steam turbinesInfo
- Publication number
- GB289427A GB289427A GB10627/28A GB1062728A GB289427A GB 289427 A GB289427 A GB 289427A GB 10627/28 A GB10627/28 A GB 10627/28A GB 1062728 A GB1062728 A GB 1062728A GB 289427 A GB289427 A GB 289427A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bolts
- radial
- holes
- carrying
- flow
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/041—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the Ljungström type
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
289,427. Aktiebolaget Ljungstr÷ms Angturbin. April 27, 1927, [Convention date]. Rotors.-In a radial flow turbine, the blade carrying discs are formed as annular elements as described in Specification 6104/09, and are connected together by bolts which are wholly or partly hollow. The object is to prevent deformation owing to temperature changes. Fig. 2 shows the application to one rotor of a combined-flow turbine of the oppositely-running rotor type. The elements 21, 22 carrying the inner ring of radial-flow blades, and the outer element 23 carrying the outer rings of radial-flow blades, and also the ring or axial-flow blades, are connected by hollow bolts 26 which pass through registering holes. The bolts are larger than the holes and must be forced in when the parts are cold, but they permit of some radial play when the parts are hot. Radial displacement of the bolts is prevented by stops 28, 31, or by other means. The sections of the bolts outside the holes may be of reduced diameter, and the bolts may have grooves 32 which may be filled with lubricant. A passage 24 is provided for drawing off or admitting driving fluid. A modification, in which two annular elements are connected, is described.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE289427X | 1927-04-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB289427A true GB289427A (en) | 1928-06-28 |
Family
ID=20307197
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB10627/28A Expired GB289427A (en) | 1927-04-27 | 1928-04-10 | Improvements in radial gas- or steam turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB289427A (en) |
-
1928
- 1928-04-10 GB GB10627/28A patent/GB289427A/en not_active Expired
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